A Design of Guidance Law of Inage Guiding Missile with Terminal Angle Constraint

LU  Ying; ZHANG  An; HE  Haifeng

doi:10.15892/j.cnki.djzdxb.2011.05.024

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (5) : 57-60. DOI: 10.15892/j.cnki.djzdxb.2011.05.024

MISSILES AND GUIDANCE TECHNOLOGY

A Design of Guidance Law of Inage Guiding Missile with Terminal Angle Constraint

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2011, 31(5): 57-60 https://doi.org/10.15892/j.cnki.djzdxb.2011.05.024

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Received	Published
2011-02-17	2011-10-20
Issue Date
2025-05-30

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